Unstructured Grid Generation and Agglomeration Multigrid Method for the Euler Solutions over Complex Aircraft Configurations
博士 === 國立成功大學 === 航空太空工程學系 === 85 === A combined Octree/Advancing-Front method is developed to generate 3-Dunstructured tetrahedral mesh. Also developed is an implicit Euler flow solver using upwind finite-volume method and agglomerationmultigrid method...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
1997
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| Online Access: | http://ndltd.ncl.edu.tw/handle/55979646037562662675 |
| Summary: | 博士 === 國立成功大學 === 航空太空工程學系 === 85 === A combined Octree/Advancing-Front method is developed to
generate 3-Dunstructured tetrahedral mesh. Also developed is an
implicit Euler flow solver using upwind finite-volume method and
agglomerationmultigrid method for convergence acceleration to
compute Euler flowover complex configurations of fighter/stores
combination.
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